AS880 PROPELLER SHAFT END - FLANGED 4.250(107.95) BOLT CIRCLE
Reaffirmed
11/19/2012
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- AS880 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY.
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DATUM A IS ROTATIONAL AXIS OF SHAFT: I. E., THE COMMON AXIS OF THOSE SHAFT FEATURES ON WHICH THE SHAFT MOUNTS AND ROTATES: E. G., SPLINES, JOURNALS, ETC.
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BREAK EDGES . 003–. 015(0. 08 – 0. 38) UNLESS OTHERWISE SPECIFIED.
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SURFACE TEXTURE: ANSI B46.1-1962. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES (3.2 MICROMETRES).
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DIMENSIONS IN INCHES(MILLIMETRES). METRIC CONVERSIONS ARE INTERNATIONAL SYSTEM UNITS (SI).
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DIMENSIONING AND TOLERANCING: ANSI Y14. 5-1966. ∅ = DIAMETER.
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FORM TOLERANCES AND THEIR RELATED DATUMS ARE RFS UNLESS OTHERWISE SPECIFIED.
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THIS AEROSPACE STANDARD SUPERSEDES AND CANCELS ARP 880.
THIS IS A DESIGN STANDARD. NOT TO BE USED AS A PART NUMBER. -
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- Citation
- SAE International Technical Standard, PROPELLER SHAFT END - FLANGED 4.250(107.95) BOLT CIRCLE, SAE Standard AS880, Reaffirmed November 2012, Issued February 1974, https://doi.org/10.4271/AS880.